B32B38/18

Tailored coefficient of thermal expansion of composite laminates using fiber steering
09738054 · 2017-08-22 · ·

Provided are assemblies, each including a first structure having a uniform coefficient of thermal expansion (CTE) and a second composite structure having a variable CTE. Also provided are methods of forming such assemblies. The second structure has overlap, transition, and baseline regions. The overlap region directly interfaces the first structure and has a CTE comparable to that of the first structure. The baseline region is away from the first structure and has a different CTE. Each of these CTEs may be uniform in its respective region. The transition region may interconnect the baseline and overlap regions and may have gradual CTE change from one end to the other. The CTE variation with the second composite structure may be achieved by changing fiber angles in at least one ply extending through all three regions. For example, any of the plies may be subjected to fiber steering.

METHOD AND SYSTEM OF PRODUCING A PLURALITY OF ANALYTICAL TEST STRIPS

A method of producing a plurality of analytical test strips using a reel-to-reel process, comprising providing at least one continuous first layer web, having disposed on a first side at least one first electrode layer, the first layer web having a first layer edge; continuously disposing at least one continuous spacer layer web onto the first side of the first layer web, wherein the spacer layer web has a spacer layer edge, wherein the disposing is position-controlled in a master-slave fashion by using a position of the first layer edge as a master position and a position of the spacer layer edge as a slave position; and continuously disposing at least one continuous second layer web onto the spacer layer web, the second layer web having disposed on a first side at least one second electrode layer, wherein the second layer web has a second layer edge.

METHOD FOR CONCEALING OPTICAL DEFECTS IN SURFACES
20220305767 · 2022-09-29 ·

A method conceals optical defects in surfaces. The method includes: obtaining a digital image by a digital optical recording the optical defect and a surrounding surface; obtaining an imitation of the surface in a region of the at least one optical defect by image processing of the digital image; printing a mirror-inverted, true-to-scale representation of the surface imitation onto a transfer film; soaking the transfer film; applying an activator onto a the transfer film or onto the surface; aligning the transfer film onto the surface so that the surface imitation on the transfer film coincides with the optical defect on the surface; pressing the transfer film onto the surface; peeling the transfer film from the surface; pressing on the ink remaining on the surface; and after complete drying of the activator and of the ink: applying a protective layer onto the surface imitation.

METHOD FOR CONCEALING OPTICAL DEFECTS IN SURFACES
20220305767 · 2022-09-29 ·

A method conceals optical defects in surfaces. The method includes: obtaining a digital image by a digital optical recording the optical defect and a surrounding surface; obtaining an imitation of the surface in a region of the at least one optical defect by image processing of the digital image; printing a mirror-inverted, true-to-scale representation of the surface imitation onto a transfer film; soaking the transfer film; applying an activator onto a the transfer film or onto the surface; aligning the transfer film onto the surface so that the surface imitation on the transfer film coincides with the optical defect on the surface; pressing the transfer film onto the surface; peeling the transfer film from the surface; pressing on the ink remaining on the surface; and after complete drying of the activator and of the ink: applying a protective layer onto the surface imitation.

Method for making a multilayer adhesive laminate
09731490 · 2017-08-15 · ·

A method allows for rapid manufacture of relatively thick adhesive coatings using a continuous process, where a single thin coating is continuously converted into a single thicker adhesive laminate. An exemplary process includes the steps of: (1) producing a web having a first surface with an adhesive layer and a second surface with a release liner; (2) slitting the web longitudinally into a first section and a second section; (3) laminating a backing film to the adhesive layer of the first section; (4) removing the release liner of the laminate of step (3) exposing the adhesive layer of the first section; and (5) laminating the second section to the laminate of step (4), wherein the adhesive layer of the laminate of step (4) is combined with the adhesive layer of the second section.

Composite cores and panels

The plurality of pieces of low density cellular material, such as foam plastics, form a core panel having opposite side surfaces and with adjacent pieces having opposing edge surfaces extending between the side surfaces. Sheets of flexible material, such as veils or mats or scrim, are adhesively attached to the side surfaces, and portions of one sheet extend between the opposing adjacent edge surfaces for limiting flexing of the panel. The pieces may be tapered, and portions of the one sheet may project between the edge surfaces either partially or fully to form double wall webs. The webs may have flanges adhesively attached to the other sheet on the opposite side. One sheet may also be stretchable in areas not adhesively attached to the pieces to provide for curving the panel from a planar position maintained by the sheet on the opposite side.

Apparatus for separating wafer from carrier

An apparatus for separating a wafer from a carrier includes a platform having an upper surface, a tape feeding unit, a first robot arm, and a controller coupled to the platform. The controller is configured to mount a wafer frame, by using the tape feeding unit, on a wafer of a wafer assembly on the upper surface of the platform. The wafer assembly includes the wafer, a carrier, and a layer of wax between the wafer and the carrier. The controller is also configured to heat the upper surface of the platform to a predetermined temperature and separate, by the first robot arm, the wafer and the wafer frame mounted thereon from the carrier.

Apparatus for separating wafer from carrier

An apparatus for separating a wafer from a carrier includes a platform having an upper surface, a tape feeding unit, a first robot arm, and a controller coupled to the platform. The controller is configured to mount a wafer frame, by using the tape feeding unit, on a wafer of a wafer assembly on the upper surface of the platform. The wafer assembly includes the wafer, a carrier, and a layer of wax between the wafer and the carrier. The controller is also configured to heat the upper surface of the platform to a predetermined temperature and separate, by the first robot arm, the wafer and the wafer frame mounted thereon from the carrier.

Material application system
09731489 · 2017-08-15 · ·

A system for applying a material to a substrate comprising: a feed section that comprises a feed roll and configured for advancing a material along a predetermined path; a material applicator roll configured to receive the material from the feed roll and apply a cut length of material to a substrate; a knife element located between the feed section and the material applicator roll; and a non-vacuum anvil roll positioned near the knife element, wherein the knife element and the non-vacuum anvil roll are positioned along the path of the material and engage the material to cut the material into the cut length of material for applying to the substrate, and wherein the material contacts the peripheral surface of the non-vacuum anvil roll only at a cut engagement point.

A Reinforced Armor And A Process For Reinforcing An Armor By Composite Layering

A reinforced armor (200) and a process for reinforcing an armor by composite layering are provided. The reinforced armor (200) includes a core structure having a strike face and a back face, a first composite fiber laminate (220) having a plurality of composite fiber plies, bonded to the strike face of the core structure, and a second composite fiber laminate (225) having a plurality of composite fiber plies, bonded to the back face of the core structure. The process for reinforcing the armor includes creating the first and second composite fiber laminates from a plurality of plies of fibrous material impregnated with a resin matrix, and bonding the first and second composite fiber laminate to both the strike face and the back face. Advantageously, the reinforced armor (200) is capable of providing protection against hazards while having a light weight compared with a rigid armor such as steel or ceramic.